Comparison of Shock-Induced Two- and Three- Dimensional Incipient Turbulent Seperation
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (4) , 534-535
- https://doi.org/10.2514/3.49750
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
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